標題: Titlebook: Dynamics of Compressible Fluids; A Textbook Oleksandr Girin Textbook 2022 The Editor(s) (if applicable) and The Author(s), under exclusive [打印本頁] 作者: memoir 時間: 2025-3-21 19:24
書目名稱Dynamics of Compressible Fluids影響因子(影響力)
書目名稱Dynamics of Compressible Fluids影響因子(影響力)學(xué)科排名
書目名稱Dynamics of Compressible Fluids網(wǎng)絡(luò)公開度
書目名稱Dynamics of Compressible Fluids網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Dynamics of Compressible Fluids被引頻次
書目名稱Dynamics of Compressible Fluids被引頻次學(xué)科排名
書目名稱Dynamics of Compressible Fluids年度引用
書目名稱Dynamics of Compressible Fluids年度引用學(xué)科排名
書目名稱Dynamics of Compressible Fluids讀者反饋
書目名稱Dynamics of Compressible Fluids讀者反饋學(xué)科排名
作者: 墊子 時間: 2025-3-21 21:54 作者: 共棲 時間: 2025-3-22 03:25
Discontinuity in?a?Gas Flowe of algebraic form of conservation laws at strong discontinuity. First, the general classification of strong discontinuities is carried out, e.g.: tangential discontinuity, contact discontinuity, shock wave, wave of a phase transition; as well, impossibility of rarefaction jumps is explained. Secon作者: 處理 時間: 2025-3-22 08:19 作者: 進步 時間: 2025-3-22 11:12
Isentropic Gas Flows with?Plane Wavesaight-line characteristics is highlighted. Equations of .- and .- simple waves and their properties are derived. Lemma of straight characteristics in a simple wave and theorem of adjoining are proved, which yields important corollary. The problem of crossing characteristics in simple compression wav作者: 萬靈丹 時間: 2025-3-22 15:25
Methods of?Wave Interaction Analysisapplied. (.,?.)-plane of states of moving gas is introduced, where (.,?.)-diagrams of simple waves and shocks are defined and plotted, together with center of diagram, compression and rarefaction branches; left-turned, right-turned wave branches being specified. The problem of breakup of arbitrary d作者: 萬靈丹 時間: 2025-3-22 20:39
Shock—Wave Flowsistics. The necessary specific issues are introduced and explained: Abel’s equation of state, covolume, effective adiabatic exponent of combustion products. Solution in simple wave domain, shell motion and velocity changing laws are obtained in analytical form. Strong point blast problem is formulat作者: 孤僻 時間: 2025-3-22 21:43 作者: Colonnade 時間: 2025-3-23 05:03 作者: Phagocytes 時間: 2025-3-23 08:47 作者: Essential 時間: 2025-3-23 12:10 作者: 你正派 時間: 2025-3-23 14:35 作者: Intact 時間: 2025-3-23 19:21
https://doi.org/10.1007/978-981-97-7232-2aight-line characteristics is highlighted. Equations of .- and .- simple waves and their properties are derived. Lemma of straight characteristics in a simple wave and theorem of adjoining are proved, which yields important corollary. The problem of crossing characteristics in simple compression wav作者: 未開化 時間: 2025-3-24 02:04 作者: 名字 時間: 2025-3-24 05:46 作者: 潰爛 時間: 2025-3-24 10:32 作者: Spina-Bifida 時間: 2025-3-24 10:49
Oleksandr GirinLeads reader from basic conservation laws via equations of multiple mathematical models to classical DCF problems.Includes the flow chocking in supersonic outflow from reservoir.Supports the reader in作者: 滔滔不絕地說 時間: 2025-3-24 18:22
http://image.papertrans.cn/e/image/284046.jpg作者: 后退 時間: 2025-3-24 20:29 作者: 大方不好 時間: 2025-3-25 03:04 作者: 花束 時間: 2025-3-25 05:57
Lecture Notes in Computer Sciencedegree of gas compression by a shock wave, determinacy of shock transition. Direct and inverse problems of the normal shock theory are described. Finally, approximate models of strong and weak shock waves are considered.作者: confide 時間: 2025-3-25 09:02 作者: garrulous 時間: 2025-3-25 12:09 作者: Talkative 時間: 2025-3-25 18:48 作者: 聯(lián)邦 時間: 2025-3-25 23:24 作者: goodwill 時間: 2025-3-26 02:57
Textbook 2022 only at velocities comparable to the speed of sound. ..Why do we study compressibility? It turns out that in order to calculate the aircraft streamlining or the internal flow in its engine, or the shell muzzle velocity, or the dynamic load of a shock wave from an accidental blast on a structural el作者: Commonplace 時間: 2025-3-26 05:31 作者: 僵硬 時間: 2025-3-26 08:31
technological devices. Unusual effects in DCM include the flow chocking in supersonic outflow from reservoirs (Sect.2.2); the shock wave formation inside an initially smooth flow (Sect.5.3); the generation of 978-3-031-11264-5978-3-031-11262-1作者: 沒血色 時間: 2025-3-26 13:59 作者: RLS898 時間: 2025-3-26 19:47 作者: gene-therapy 時間: 2025-3-26 21:07
Governing Equations and?Initial-Boundary-Value Problems of special type are also formulated. The characteristics as potential branch-lines of solution and as a trajectory of possible weak discontinuities are discussed; relations along weak discontinuity are obtained. Problem of disintegration of arbitrary weak discontinuity is set and non-evolutionary c作者: Adulterate 時間: 2025-3-27 03:11 作者: 隱士 時間: 2025-3-27 08:38
Shock—Wave Flowslems of wave interactions yielding the wave effects are also considered: shock tube performance, the tube design, direct and inverse problems; shock wave reflection from rigid wall with amplification of its percussive action; shock wave interaction with contact surface; interaction of two shocks; sh作者: monopoly 時間: 2025-3-27 12:46 作者: BAIT 時間: 2025-3-27 13:57 作者: Mets552 時間: 2025-3-27 20:36
Cerebral Blood Flow Mapping the Brain,voir. Instead, to increase the flow velocity, one needs to apply a special nozzle. Subsonic (Venturi tube) and supersonic (Laval nozzle) outflow modes are considered. Nozzle calculation schemes are described; on-design and off-design nozzles are defined.作者: GLUE 時間: 2025-3-27 22:40 作者: ULCER 時間: 2025-3-28 03:41
Lecture Notes in Computer Scienceimilar solution, which gives complete analysis of all solution cases where the final equilibrium state is found. System of equations for the sought waves and logic of the root finding are added. Description of a simpler acoustic approximation is given.作者: 不可侵犯 時間: 2025-3-28 08:03 作者: 魔鬼在游行 時間: 2025-3-28 12:00
Jing He,Zhen Zhang,Yuanhui Xiao,Mian Wangction is found; steady expansion into vacuum is described as a limiting case. Plane supersonic outflow from a slit is described with “barrel”-flow formation bounded by free-surface. Main concepts of thin airfoil theory and problem formulation are listed. Thin profile streamlining in subsonic and sup作者: insipid 時間: 2025-3-28 15:31
10樓作者: GUILT 時間: 2025-3-28 21:15
10樓作者: 尖酸一點 時間: 2025-3-28 23:42
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